An integrally bladed rotor disk (20) for a turbine comprises rotor blades (40), which are bonded to a disk element (30), and a sealing device (60) for suppressing or reducing a transfer of cooling air from a high pressure side (12) of the rotor disk (20) through openings (24) at the rotor disk (20) to the low pressure side (14) of the rotor disk (20).
申请公布号
WO2010088882(A3)
申请公布日期
2011.02.24
申请号
WO2010DE00107
申请日期
2010.02.01
申请人
MTU AERO ENGINES GMBH;BORUFKA, HANS-PETER;STIEHLER, FRANK;ARRIETA, HERNAN, VICTOR;PROKOPCZUK, PATRICK;LORENZ, JOACHIM
发明人
BORUFKA, HANS-PETER;STIEHLER, FRANK;ARRIETA, HERNAN, VICTOR;PROKOPCZUK, PATRICK;LORENZ, JOACHIM
